Boeing 727-25C

Service difficulty reports · 2,007

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '72725C'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS203595Shear Web · corrodedWHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON SHEAR WEB AND HAT CHANNEL AT BS 1173, LBL 23 TO 28 WL 208. REPLACED HAT CHANNEL AND WEB IAW SRM 57-10-2, 51-30-2, 51-30-8, 51-40-2, 53-10-1.Jun 16, 1995 · N950UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203594Rib · crackedWHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACKED SUPPORT RIB ON RT HORIZ STAB T/E AT STA 99.79. REPLACED RIB IAW SRM 51-20-4, 51-20-5, 57-30-2, M/M 27-30-5.Jun 16, 1995 · N950UP · Boeing 72725C · Horizontal Stabilizer, Spar/RibSDR UPS203593Skin · delaminatedWHILE IN FOR C-CHECK MAINTENANCE, FOUND DELAMINATION ON R/W O/B AFT FLAP ON UPPER SKIN 14 INCHES FROM I/B SIDE. REPAIRED IAW SRM 51-40-06.Jun 16, 1995 · N950UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203592Skin · lightning strikeWHILE IN FOR C-CHECK MAINTENANCE, FOUND DAMAGE TO SKIN DUE TO LIGHTNING AT STA 400, STR 4 LT. REPAIRED IAW SRM 53-30-3, 51-10-2, 51-30-2, 51-20-4.Jun 16, 1995 · N950UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS203591Skin · crackedWHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACK ON EXTERNAL SKIN AT BS 1228, RBL 9 WL 148. REPAIRED IAW SRM 53-30-3.Jun 16, 1995 · N950UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS203590Bulkhead · crackedWHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACK ON BULKHEAD BS 178, RBL 1 WL 197. REAPIRED IAW SRM 53-10-9, 53-10-2.Jun 16, 1995 · N950UP · Boeing 72725C · Fuselage Main, BulkheadSDR UPS203512Guide Hooks · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKED AND WORN NR 1 SLAT I/B GUIDE HOOK. INSTALLED FABRICATED PARTS IAW SRM 57-50-3, 51-30-2, M/M 27-81-0.Jun 12, 1995 · N951UP · Boeing 72725C · Leading Edge DevicesSDR UPS203511Guide Hooks · crackedWHILE IN C-CHECK, MAINTENANCE FOUND WORN AND CRACKED NR 5 SLAT GUIDE HOOKS. INSTALLED FABRICATED PARTS IAW SRM 57-30-3, M/M 27-81-11.Jun 12, 1995 · N951UP · Boeing 72725C · Leading Edge DevicesSDR UPS203510Chord · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON RT UPPER NOSE CHORD STA 329, RBL 13, WL 170. REPAIRED IAW EO 727-53-1617.Jun 12, 1995 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203502Chord · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LT UPPER NOSE CHORD AT STA 318, LBL 13, WL 170. REPLACED CHORD IAW SRM 51-30-2.Jun 9, 1995 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203501Floorbeam · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER AND LOWER FLOORBEAM AT STA 1130, RBL 25, WL 200 TO 208. REPAIRED IAW EO 727-53-1614, SRM 51-10-1.Jun 9, 1995 · N951UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS203500Skin · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B FLAP AT I/B END UPPER SURFACE. REPAIRED IAW SRM 51-40-6.Jun 9, 1995 · N951UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203499Web · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AT STA 1110 THROUGH 1130, RBL 45, WL 200. INSTALLED FABRICATED PARTS IAW SRM 51-20-1, 51-20-4, 51-30-2.Jun 9, 1995 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203498Flap Track · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 5 FLAP TRACK. INSTALLED NEW TRACK IAW M/M 27-51-31.Jun 9, 1995 · N951UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203497Web · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AT STA 1110 THROUGH 1130, RBL 25, WL 200. INSTALLED FABRICATED PARTS IAW SRM 53-10-2, 51-20-1, 51-30-2, 51-10-2, M/M 51-20-151.Jun 9, 1995 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203488Skin · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AND CRACKS ON LOWER FUEL CELL SKIN AT STA 740, RBL 1-15. REPAIRED IAW E.O. B727-5710-7079A.Jun 8, 1995 · N948UP · Boeing 72725C · Wing, Plate/SkinSDR UPS203487Spar Chord · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER FRONT SPAR CHORD AT STA. 740, WL 166.5, BL 0. REPLACED CHORD IAW E.O. B727-5710-7078A.Jun 8, 1995 · N948UP · Boeing 72725C · Wing SparSDR UPS203486Skin · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND RT WING NR 6 K-FLAP BULLNOSE O/B HINGE UPPER SURFACE OF UPPER ATTACH POINTS HAVE CORROSION. INSTALLED FABRICATED PARTS IAW SRM 57-50-1, 51-10-6, 51-10-1, 51-20-04.Jun 8, 1995 · N948UP · Boeing 72725C · Leading Edge DevicesSDR 95FDEA00858Fitting · crackedMAIN CARGO DOOR AFT CAM SUPPORT FITTING CRACKED. REPLACED FITTING WITH 65-26680-5 IN PLACE OF ORIGINAL - 3 FITTINGS OBSOLETE PER EA NR 7-5230-25056.Jun 8, 1995 · N134FE · Boeing 72725C · Cargo/Baggage DoorsSDR 95FDEA00857Fitting · crackedRIGHT STA 870 CRACK ABOVE STR 10 EXTENDING UNDER SPLICE PLATE - AFT SIDE OF 870 FORGING. REPAIRED BS 870 TERMINAL FITTING AS PER BOEING SB 727-53-0.Jun 8, 1995 · N134FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203461Skin · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER FUEL CELL SKIN STA. 740, LBL 39 AND 45. REPAIRED IAW E.O. 727-5710-7079A.Jun 7, 1995 · N948UP · Boeing 72725C · Wing, Plate/SkinSDR UPS203460Skin · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FUEL CELL SKIN B.S. 850-870, RBL 45-65. REPAIRED IAW E.O. 727-57-1385.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS203457K-Flap · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP. REPLACED IAW M/M 27-81-1.Jun 7, 1995 · N948UP · Boeing 72725C · Leading Edge DevicesSDR UPS203456Skin · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FUEL SKIN AT B.S. 870, RBL 32-39, WL 188. REPAIRED IAW E.O. 727-57-1386.Jun 7, 1995 · N948UP · Boeing 72725C · Wing, Plate/SkinSDR UPS203455Expansion Link · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSEAGE TO WING CENTER SECTION EXPANSION LINKS (LT AND RT) AT B.S. 740, RBL 13, LBL 13, WL 150.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203454Spar Chord · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SPAR CHORD B.S. 870, RBL 35, WL 188. REPAIRED IAW E.O. B727-5710-7063A.Jun 7, 1995 · N948UP · Boeing 72725C · Wing SparSDR UPS203453Skin · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKS AROUND FASTENERS (HIGH FREQUENCY EDDY CURRENT INSPECTION) AT B.S. 259.5 TO 272, STR 9R, WINDSHIELD UPPER SILL. REPAIRED IAW SRM 51-30-2, 53-30-3.Jun 7, 1995 · N948UP · Boeing 72725C · Wing, Plate/SkinSDR UPS203452Tab · delaminationWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B AILERON TAB. REPAIRED IAW SRM 51-40-6.Jun 7, 1995 · N948UP · Boeing 72725C · Aileron TabsSDR UPS203451Tab · delaminationWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B AILERON TAB. REPAIRED IAW SRM 51-40-6.Jun 7, 1995 · N948UP · Boeing 72725C · Aileron TabsSDR UPS203450K-Flap · corrodedWHILE IN C-CHECK MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP. REPLACED IAW M/M 27-81-1.Jun 7, 1995 · N948UP · Boeing 72725C · Leading Edge DevicesSDR UPS203449K-Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 K-FLAP. REPLACED IAW M/M 27-81-1.Jun 7, 1995 · N948UP · Boeing 72725C · Leading Edge DevicesSDR UPS203448Web · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AT B.S. 294-350, LBL 14, WL 180-160. INSTALLED FABRICATED PARTS IAW E.O 727-53-1612.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203447Chord · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD B.S. 294-350, LBL 15, WL 169. REPLACED IAW SRM 51-30-5, 51-30-2.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203446Web · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AROUND LOCKBOLT STA 259.5, LBL 21, WL 192.5. REPAIRED IAW SRM 51-40-2, 51-10-2, 51-30-2, 53-10-2.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203445Rib · crackedWHILE IN C-CHECK, MAINTENANCE FOUND RT ELEVATOR SUPPORT RIB AT STA 99.79 IS CRACKED. REPLACED RIB IAW SRM 51-30-2.Jun 7, 1995 · N948UP · Boeing 72725C · Elevator, Spar/RibSDR UPS203444Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B MID FLAP T/E WEDGE 7 INCHES FROM O/B END ON LOWER SURFACE. REPAIRED IAW SRM 51-40-6.Jun 7, 1995 · N948UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203443Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B MID FLAP T/E WEDGE ON O/B CORNER. REPAIRED IAW SRM 51-40-6.Jun 7, 1995 · N948UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203442Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B MID FLAP T/E WEDGE 27 INCHES FROM I/B END. REPAIRED IAW SRM 51-40-6.Jun 7, 1995 · N948UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203441Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B MID FLAP T/E WEDGE 36 INCHES FROM I/B END. REPAIRED IAW SRM 51-40-6.Jun 7, 1995 · N948UP · Boeing 72725C · Trailing Edge FlapsSDR UPS203440Seat Track · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK WELL AND TABS B.S. 1130-1135, RBL 45, WL 208. REPLACED TRACK IAW SRM 53-10-5, 53-10-2, 51-30-2, M/M 51-20-151.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS203439Seat Track · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN SEAT TRACK B.S. 580, RBL 65, WL 208. REPLACED TRACK IAW SRM 51-30-2.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS203438Seat Track · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK WELL B.S. 697-703, LBL 65, WL 208. INSTALLED NEW TRACK STA. 620-740 IAW SRM 53-10-1, 51-30-2.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS203437Stiffener · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER B.S. 308, LBL 12 TO RBL 12 WL 180. REPLACED STIFFENER IAW SRM 53-10-1, 51-10-1.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203436Stiffener · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER B.S. 301, LBL 12 TO RBL 12 WL 180. REPLACED STIFFENER IAW SRM 53-10-1, 51-10-1, 51-30-2.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203435Web · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR WEB STA 1170, RBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-40-2, 51-30-8, 51-10-2, 51-30-2, M/M 51-20-151.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203434Hat Channel · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON HAT CHANNEL STA 1145-1148, RBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-10-2, 51-20-4, 51-30-6, 51-10-1.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS203433Seat Track · corrodedWHILE IN C-CHECK MAINTENANCE FOUND CORROSION ON SEAT TRACK TABS I/B AND O/B B.S. 595 TO 600, LBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 53-10-1, 53-10-5.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS203432Angle · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON ANGLE AT B.S. 280, WL 177 NOSE WHEELWELL. INSTALLED FABRICATED PARTS IAW SRM 53-10-1, 51-20-1, 53-30-2.Jun 7, 1995 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA00856Floor Beam · corrodedCORROSION ON TOP OF LEG ON FLOORBEAM (TOP LEG) STA 480 RBL 18-20. BLENDED OUT CORROSION ON TOP LEG OF FLOORBEAM, BLENDED OUT AREA 2.0 INCHES X .75 INCH WIDE, AT A DEPTH OF .045 INCH EXCEEDING SRM LIMITS. INSTALLED STRAP REPAIR PER ESO 11782 DATED 6-13-95 EA Jun 7, 1995 · N134FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA00854Spar Web · corrodedCENTER WING BOX AFT SPAR WEB SKIN AT UPPER CHORD HAS FOUR EACH FASTENERS WITH POPPED HEADS AND ONE READY TO POP, TOTAL FIVE. WEB SKIN IS BULGED AT APPROX RBL 50. REMOVED RIVETS AND CUT OUT TOP PORTION OF WEB OUT TO REMOVE CORROSION ON UPPER SPAR. INSTALLED Jun 7, 1995 · N134FE · Boeing 72725C · Wing Spar
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